Heterodyne starring array active imager with spread spectrum illuminator

ABSTRACT

A heterodyne starring array active imager for producing an image. The imager comprises a light source and a component for segregating the light into frequency bands, each band intermittently illuminating a region of a scene and an array of light collecting sites, each comprising: a coupling component optically coupling scene light into a first waveguide and a local oscillator light coupled into a second waveguide. First and second waveguides coupled to a third waveguide with scene light and local oscillator light propagating into the third waveguide. A square law photo detector at each light collecting site receives the merged light for heterodyning the scene light and the local oscillator light. Components receive and process the heterodyned light from the photo detectors to produce a frame signal for each light collecting site. A read-out device produces an array signal responsive to the frame signal from each light collecting site.

CROSS REFERENCE TO RELATED APPLICATIONS

The present application is a continuation-in-part application claimingpriority to a non-provisional application filed on Aug. 22, 2019,entitled Heterodyne Starring Array Active Imager, and assignedapplication Ser. No. 16/548,757, now U.S. Pat. No. 10,587,347, whichclaims priority to a provisional application filed on Aug. 22, 2018,entitled Heterodyne Starring Array Imager, assigned application No.62/720,978. Both applications are incorporated by reference herein.

FIELD OF THE INVENTION

The present disclosure relates to imaging, and more particularly tosystems and methods for heterodyne detection of active radiation in astarring imager configuration.

OBJECT OF THE INVENTION

There is a long felt need both commercially and by the military forsmall, inexpensive, power efficient, eye-safe, and solid-state activeimagers that provide range-gated imagery plus accurate pixel-by-pixelrange that is unaffected by bright sunlit backgrounds.

The continuation-in-part application adds an alternative embodiment thatcomprises an illuminator that does not require an external opticalcavity to tailor its spectral bandwidth and modifies the HSAAI photonicsarray to accommodate the fact that the illuminator spectrum varies overthe field of view.

The object of the invention set forth in the continuation-in-partapplication is to reduce production cost and risk by employing a simplerand more rugged illuminator design.

Also, using the illuminator disclosed herein reduces the photo detectortemporal bandwidth, thereby improving photonics array producibility andallowing more options for the photo detector electronics processing.

Further, the alternative embodiment described by thecontinuation-in-part application reduces the amount of scattered lightseen by the HSAAI imager when used in poor atmospheric conditions,thereby improving the ability to see through fog, rain, snow, smoke, andother scattering media.

BACKGROUND DESCRIPTION OF THE PRIOR ART

U.S. Pat. No. 7,995,191 B1 to Sandusky (hereinafter “Sandusky”) andassigned to Sandia Corporation discloses a scannerless 3-D imagingapparatus which utilizes an amplitude modulated continuous wave lightsource to illuminate a field of view containing a desired target.Backscattered light from the target is passed through one or more lossmodulators which are modulated at the same frequency as the lightsource, but with a phase delay δ which can be fixed or variable. Thebackscattered light is demodulated by the loss modulator and detectedwith a CCD, CMOS or focal plane array (FPA) detector to construct a 3-Dimage of the target. The scannerless 3-D imaging apparatus, which canoperate in the eye-safe wavelength region 1.4-1.7 μm and which can beconstructed as a flash LADAR, has applications for vehicle collisionavoidance, autonomous rendezvous and docking, robotic vision, industrialinspection and measurement, 3-D cameras, and facial recognition.

Unlike the current invention, Sandusky applies only to active imagingand does not use heterodyning. Passive imagery is not sensed at all. Foractive imaging, Sandusky does not have the background light immunityadvantages of HSAAI the Heterodyne Starring Array Active Imager (HSAAI)and is not multi-spectral.

U.S. Patent Application Pub. No. US 2005/0046857 A1 to Bingham et al.(hereinafter “Bingham”) discloses systems and methods forspatial-heterodyne interferometry for transmission (SHIFT) measurements.A method includes digitally recording a spatially heterodyned hologramincluding spatial heterodyne fringes for Fourier analysis using areference beam, and an object beam that is transmitted through an objectthat is at least partially translucent; Fourier analyzing the digitallyrecorded spatially-heterodyned hologram, by shifting an original originof the digitally recorded spatially-heterodyned hologram to sit on topof a spatial-heterodyne carrier frequency defined by an angle betweenthe reference beam and the object beam, to define an analyzed image;digitally filtering the analyzed image to cut off signals around theoriginal origin to define a result; and performing an inverse Fouriertransform on the result.

Bingham uses heterodyning in the sense of mixing beams for a hologramapplication but does not use photo detectors or waveguide technology.Further, the objective of Bingham is interferometry and not imaging, andreal-time multi-spectral narrow band imagery with high sensitivity isnot provided. Both the apparatus and objective are very different fromthe invention described in this application. In addition, Bingham doesnot provide any passive imagery.

U.S. Pat. No. 6,664,529 B2 to Pack et al. and assigned to Utah StateUniversity (hereinafter “Pack”) discloses a 3D Multispectral Lidar. Thesystem comprises a laser transmitter light source, a laser detectionassembly, optics that couple the outgoing and incoming laser signals, adigital camera assembly for collecting passive light, a position andorientation system, and processing hardware. The system providesreal-time georectified three dimensional images and topography using anairborne platform. The system collects time-synchronous Lidar range andimage data in an optical receiver. The individual images are thenmosaiced and orthorectified in real-time. The Lidar range data and imagedata are then coupled to a position and orientation system to transformthe three-dimensional range images to a single geographically referencedmultispectral three-dimensional image

Pack includes direct detection passive imaging and does not employeither waveguide technology or heterodyning. Pack does not provide themulti-spectral and highly sensitive imagery of the invention describedin this application.

U.S. Pat. No. 7,049,597 B2 to Bodkin (hereinafter “Bodkin”) discloses acommon aperture, multi-mode optical imager for imaging electromagneticradiation bands from a field of two or more different wavelengths isdescribed. Fore-optics are provided to gather and direct electromagneticradiation bands forming an image into an aperture of the multi-modeoptical imager. The image is divided into two different wavelengthbands, such as visible light and long-wave infrared. The firstwavelength band (e.g., visible light) is detected by a first detector,such as a CCD array, for imaging thereof. The second wavelength band(e.g., long-wave infrared) is detected by a second detector, such as anuncooled microbolometer array, for imaging thereof. Additional opticsmay be provided for conditioning of the first and second wavelengthbands, such as such as for changing the magnification, providing coldshielding, filtering, and/or further spectral separation.

Bodkin uses direct detection and not heterodyning and does not providethe sensitivity or ability to image very narrow spectral bands that isprovided by the invention described in this application. Further, themultiple spectral bands are independently imaged on separate detectorarrays rather than gathered by optical collection elements andwaveguided to spectral filters and then to heterodyned detectors. Thecurrent invention HSAAI provides the capability to switch spectral bandselection, the ability to image many and not just two spectral bands,and sensitivity for narrow spectral bands not possible with the directdetection method of the App.

U.S. Pat. No. 6,931,031 B2 to Williams et al. and assigned to AstonUniversity (hereinafter “Williams”) discloses a dual wavelength opticalfiber distributed feedback laser comprising a pump laser coupled to abirefringent fiber in which a first grating device (two co-locatedsingle phase-shift fiber Bragg gratings (FBGs)) is provided. The gratingdevice gives the laser two potential lasing modes in each of twoorthogonal polarization states. A polarization mode coupling FBG selectstwo orthogonally polarized modes on which the laser oscillates. In aphotonic data carrying signal source, the laser is coupled to apolarization dependent, optical modulator operable to apply amodulation, at a data signal frequency, to one polarization mode of thelaser output. In an optical waveguide based electronic signaltransmission system the modulated and unmodulated polarization modesoutput from the source are transmitted across a fiber transmission lineto a polarizing optical fiber in which the two modes heterodyne togenerate an electronic carrier signal in the optical domain.

Williams uses some of the same basic tools as the current invention likeBragg gratings and waveguide modulators. However, the objective iscompletely different in that these components are used for thegeneration of laser light and not for imaging. Further, the basic toolset (spectral filtering, waveguiding in fibers) is implemented verydifferently to address the different objective.

U.S. Pat. No. 5,146,358 to Brooks and assigned to PYR Systems, Inc.(hereinafter “Brooks”) discloses an optical communication system fordisseminating information. The systems include a source of continuouswave laser light and one or more acoustic beams which are frequency oramplitude modulated by data. The laser light beam and the acoustic beamsare input to an acousto-optical modulator for producing an undiffractedlaser light beam and one or more diffracted laser light beams. Thediffracted laser light beams are frequency shifted from the undiffractedlaser light beam and contain the data to be transmitted. The diffractedand undiffracted beams are combined and transmitted over an opticalfiber for demodulation at a distant location by a receiver. The receiverincludes a photodiode which heterodynes the diffracted and undiffractedbeams and produces signals having the frequencies of the acoustic beams.Tuning circuitry separates the signals and demodulators reconstruct thedata transmitted. By using two such communication systems with a singleoptical fiber and by allocating the available bandwidth, simultaneous,bidirectional multi-channel communications are achieved.

Brooks uses many of the same component parts as the invention describedin this application but the objective and implementation of Brooks isvery different. Brooks addresses communications and not imaging and doesnot use heterodyning in photo detectors to provide highly sensitive,multi-spectral images.

U.S. Pat. No. 7,667,824 issued to Moran discloses a range-gatedsphearography system and related methods that includes at least oneimaging detector coupled to a laser light source.

Moran implements surface vibration sensing by employing range gatedtechniques along with interferometers. Aside from implementing adifferent function than HSAAI, Moran does not use heterodyning, does notimplement a starring array, and cannot be used for passive imaging.

U.S. Pat. No. 7,449,673 issued to Chuang, et al. discloses a system andmethod for reducing peak power of a laser pulse and reducing specklecontrast of a single pulse comprising a plurality of elements orientedso as to split a pulse or pulses transmitted from a light source.

Chuang achieves one of many benefits of HSAAI, namely reduction ofspeckle in active imagery. However, implementation is via splitting ofoptical beams, so the method is very different from HSAAI. In addition,other benefits of HSAAI are not disclosed in Chuang.

U.S. Pat. No. 7,233,392 issued to Margalith, et al. discloses a spectralimaging device including a optical parametric oscillator that can betuned across a wide range of wavelengths while illuminating a target.

While HSAAI shares the ability to vary wavelength of operation, thewaveguide method used in HSAAI is different from Margalith. Also, HSAAIdiscloses other benefits, like heterodyne detection.

General waveguide technology is also prior art. Of the several waveguidetechnologies available to implement the HSAAI, silicon is the mostmature. The silicon waveguide technology was originally developed toimplement fiber optic communications. Component parts developed andtested include light collectors that gather free-air light into awaveguide, waveguide designs that can turn sharp corners and be overlaidat right angles without cross-talk, polarization diversifiers to convertinput light into one electromagnetic mode for waveguide transmission,interferometers that can also be used as optical switches, spectralresonators (generally in the form of one or more rings or racetracks),efficient light splitters and couplers, and waveguide-to-photo detectorinterfaces that currently provide a 60 Gigahertz (GHz) temporalbandwidth.

SUMMARY OF THE INVENTION

None of the prior art taken individually or collectively discloses andteaches a method comprising illuminating the scene by pulsing a laserdiode, a light emitting diode, a laser, or another light source andcommunicating scene return light with a heterodyned starringgated-sensor to reduce the effect of background and dark current inducedshot noise and eliminate speckle. None of the prior art takenindividually or collectively discloses an apparatus with the activeimaging technical advantages and benefits of the present invention.

The present invention uses a variety of waveguide components toimplement heterodyne sensing in a starring array format. The knownwaveguide art is too diverse and has too many varieties to list, but theavailability and conventional functionality of the waveguide componentsused in the current invention are known to those skilled in the art,albeit assembled into a novel and non-obvious system of the presentinvention.

Various methods for synchronizing an optical emitter with an opticalreceiver and using time-of-flight of the light to implement ranging arewell known to experts in the field. The HSAAI invention uses a novelheterodyne photo detection implementation to mitigate the major noisesources that limit time-of-flight imaging performance. The HSAAIinvention also uses a novel means for gating the optical receiver (thatis, raising or lowering receiver sensitivity) during illuminator lightemission.

HSAAI uses continuous wave laser diodes (CWLD) as illuminators. The“continuous” in CWLD refers to the type of diode and not the duty cycleof the light. CWLD are constructed differently than high peak powerlaser diodes (PPLD) that are designed to operate for only a short pulseperiod. CWLD can be pulsed continually without regard to duty cycle.PPLD are generally restricted to a duty cycle of approximately 0.02.

The limited pulse repetition rate of the peak illuminators leads toseveral performance problems. Speckle is a disturbing image artifactthat is eliminated by summing ten or more pulses that return from eachobject in the scene. A video rate of 60 frames per second is generallydesired in an imager, each frame requiring ten pulses to eliminatespeckle. Further, most applications require either long range gates orthe ability to visit many ranges each frame. Other than large andexpensive laser sources, current PPLD technology does not provide boththe peak power plus the high pulse repetition rate needed for manyapplications.

CWLD provides the high repetition rate needed for speckle reduction atvideo rates with many range gates. However, when direct detection isused, the signal-to-noise ratio is poor. CWLD provides too little energyper pulse to use direct detection, especially during the day againstsunlit backgrounds.

Heterodyning solves the signal-to-noise problem. CWLD illuminatorscoupled with HSAAI receivers provide signals with a high signal-to-noiseratio and speckle free imagery over extended range gates.

For multi-pulse imaging, the duration of the laser pulse is set by

$t_{laser} = \frac{2\left( {R_{\max} - R_{DZ}} \right)}{c}$

where c is the speed of light. R_(max) is the longest effective rangefor a particular operating environment. It is set by the observer anddepends on field conditions. R_(DZ) is a dark zone that is needed tolimit the dynamic range of the imager and to avoid light scattered bynearby airborne particulates. It is created by the delay t_(DZ) betweenthe end of the laser light pulse and the beginning of focal plane array(FPA) light integration. t_(DZ) is also needed to clear the detectors ofany signal generated during laser light emission.

Laser pulse duration t_(laser) t is the duration from the current laserpulse to the previously stored charge. Thus, the laser's duty cycle,D_(cycle), is

${D_{cycle} = \frac{t_{laser}}{{2t_{laser}} + t_{DZ}}}.$The only range R_(ng) for which the focal plane array (FPA) integrates100% of the laser light is R_(max). Thus, the duty cycle of the FPA,D_(FPA), at closer ranges is

$D_{FPA} = {{\frac{R_{ng} - R_{DZ}}{R_{\max} - R_{DZ}}\mspace{14mu}{for}\mspace{14mu}{RDZ}} \leq {Rng} \leq {{R\max}.}}$The effect of D_(FPA) is that apparent illumination falls offproportional to range and not range-squared. Notice two things about themulti-pulse apparent irradiance. First, ground irradiance is fullyutilized by the imager at the user-selected Rmax range. Second,effective illumination versus range is more uniform with multi-pulsethan single-pulse; search and target acquisition are much easier withmulti-pulse.

This disclosure describes the implementation of a two-dimensional arrayof heterodyned photo receptors, designated as light collection sites(LCS). The array size is M by N, where M and N are integers, and eachinteger can have a value between one and many thousands.

Implementation of an imaging camera providing M by N display pixelsrequires circuitry for synchronization, global or progressive shutterlogic, row and column read-out, analog-to-digital conversion,non-uniformity corrections, and display formatting, to name some of thenecessary functions. Certain of these required camera functions are wellknown to those skilled in the camera art, and a description of theimplementation of many necessary camera functions is not provided inthis disclosure.

The focus of the explanatory material in this disclosure is thereforedescribing the implementation of the LCS that enables heterodyne sensingin a starring array format.

The HSAAI of the present invention separates the light collectionprocess from the photo detection process. Sometimes photo detection isreferred to herein as simply detection. In the detection or photodetection process, light waves input to the photo detector are convertedto electrical signals for further processing. That is, a two-dimensionalarray of light collection sites (LCS) is situated in the image plane ofan objective lens. Each LCS contains an air-to-waveguide light couplerthat conveys collected light into a waveguide within the LCS. In someembodiments, the light is conveyed to a polarization diversifier or amulti-mode-to-single mode converter and then into the waveguide.

Efficient heterodyning is implemented using waveguides to convey localoscillator light to each LCS, and at each LCS combining scene and localoscillator light streams in the LCS waveguide prior to heterodyning,which occurs during photo detection within each LCS. Combining the lightstreams in a waveguide prior to photo detection ensures good electric(E) field alignment and phase-front matching and therefore efficientheterodyning. In an alternative embodiment the photo detector is locatedremotely and can thereby service multiple LCSs.

Separating light collection from photo detection results in efficientheterodyning for two reasons. First, collecting light into a waveguideenables polarization diversification of the scene light; that is, mostof the arriving scene light is converted to the polarization that willbe used during heterodyning. Second, combining the local oscillatorlight and scene light in a waveguide prior to photo detection ensuresefficient mixing of the light streams and alignment of phase fronts.

The HSAAI of the present invention also solves two problems associatedwith using small and power efficient continuous wave laser diode (CWLD)as gated illuminators for active imaging. Using low peak power laserdiodes requires long dwell times to compensate for the low energy ineach laser diode pulse. When heterodyne sensing is used, rather thandirect detection, the output signal is proportional to the heterodyneshot noise, so the local oscillator amplitude is raised, making othersystem noises unimportant. Also, the wide spectral bandwidth associatedwith sunlight cannot produce a significant heterodyne signal. CWLDilluminators and heterodyne receivers therefore provide a low volume,low weight, highly power efficient active imager combination asdescribed and claimed herein. Because CWLDs emit little energy whenpulsed quickly, active imagers using CWLDs must collect the lightreturns from many laser pulses before outputting an image frame. Eachtime the CWLD is pulsed, however, the photo detector must be shieldedfrom the bright back scatter produced by nearby objects and theatmosphere when illuminated by the laser pulse. Thus, the HSAAI of thepresent invention provides two means of interrupting the detector lightstream without affecting the signal already integrated by the photodetector circuit. One technique uses an optical switch, such as a MachZehnder interferometer, in the LCS waveguide; the switch blocks receivedlight during CWLD pulse emissions. A second technique, preferred overthe first technique or used in combination with the first technique, isto slightly offset the wavelength of the local oscillator while theilluminator is emitting and for a short period thereafter, therebycreating a desired dark zone in the front of the imager so that brightreflections do not blind the camera. The local oscillator intensity isnot varied when the wavelength is shifted, so the photodetector does notexperience a direct current (DC) amplitude change. However, shifting thelocal oscillator frequency/wavelength results in shifting the heterodynesignal out of the photo detector temporal bandwidth.

The descriptions herein of each LCS are meant as “building blocks” witheach block used, not used, or used many times as needed to optimize thefinal HSAAI design.

In another embodiment (sometimes referred to as a second or alternativeembodiment), as described and claimed in the continuation-in-partapplication, a method for using spectrally broadband light as anilluminator for the HSAAI is described.

The illuminator and receiver must act in unison to implement an activeimager. The preferred HSAAI embodiment, as described in FIGS. 1-9,comprises the HSAAI imager used with any available illuminator thatemits light with a sufficiently small spectral bandwidth. Thealternative embodiment (set forth in FIGS. 10-13) describes a spectrallybroadband illuminator and the functional and component changes requiredin the preferred embodiment of the HSAAI to operate with the broadbandilluminator, while illuminating the scene with a spectrally-narrowsignal.

Heterodyne sensing involves imaging laser light reflected from a sceneand simultaneously irradiating square law photo detectors with a localoscillator signal. The sum of the temporal frequency bandwidths of thescene illumination and local oscillator must be within the operationaltemporal bandwidth of the photo detector. That typically means usingvery narrow band laser illumination, and generating that kind of lightwith the necessary power can be difficult. This disclosure of thealternative embodiment implements a method and associated system wherebythe laser spectrum generated by raw laser diodes can be used forillumination without the need for external optical cavities to narrowthe light spectrum generated by the laser diode.

A diffraction grating or optical prism is used to spread the laser diodeilluminator light over a field of view. The illuminator light at eachposition in the field of view, that is the light that is reflected fromeach scene object, is therefore spectrally narrow band, and it varies inspectral content at each location across the field of view.

Spectral filters are included within the HSAAI photonics array in orderto generate the array of local oscillator wavelengths that are needed toheterodyne the different wavelengths of illuminator light reflected fromdifferent field-of-view locations.

BRIEF DESCRIPTION OF THE DRAWINGS

A more complete understanding of these embodiments, and the attendantadvantages and features thereof, will be more readily understood byreference to the following detailed description when considered inconjunction with the accompanying drawing. The drawings described hereinare for illustrative purposes only of selected embodiments and not allpossible apparatus configurations and are not intended to limit thescope of the present disclosure. The invention has the potential to beconfigured in multiple versions so as to generate superior technicalperformance in any given application. Therefore, it is understood thatin some configurations not all elements will always be necessary for thespecific embodiment or implementation of the invention. It should alsobe apparent that there is no restrictive one-to-one correspondencebetween any given embodiment of the invention and the elements in thedrawing.

For clarity and in order to emphasize certain features, all of theinvention features are not shown in the drawing, and all of the featuresthat might be included in the drawing are not necessary for everyspecific embodiment of the invention. The invention also encompassesembodiments that combine features illustrated in the drawing;embodiments that omit, modify, or replace some of the features depicted;and embodiments that include features not illustrated in the drawing.

As used herein, relational terms, such as “first” and “second,” “top”and “bottom,” and the like, may be used solely to distinguish one entityor element from another entity or element without necessarily requiringor implying any physical or logical relationship or order between suchentities or elements.

The drawing is integral to the application and is included by way ofillustrating the HSAAI apparatus.

FIG. 1 illustrates the components associated with the heterodyne processat each light collection site (LCS).

FIG. 2 illustrates wavelength relationships when heterodyning.

FIG. 3 depicts components of the photo detector output electronicsaccording to one embodiment.

FIG. 4 illustrates a horn coupler used to couple free-air light from anobjective lens into a waveguide.

FIG. 5 illustrates a Bragg grating that can also be used to couple thelight form an objective lens into a waveguide. Either a Bragg grating ora horn coupler, not both, would be used in each LCS.

FIG. 6 illustrates a Mach Zehnder interferometer that can also be usedas an optical switch.

FIG. 6 shows the inclusion of a PIN diode to control the optical pathlength of one interferometer arm so that switching operation can beoptimized for a selected wavelength.

FIG. 7 illustrates operation of an active imager LCS.

FIG. 8 illustrates the LCS with a Mach Zehnder interferometer added asan optical switch to help reduce backscatter signal during illuminatoremission.

FIG. 9 illustrates an optical system that uses a diffraction grating tospread broadband illuminator light at different angles over a field ofview.

FIG. 10 illustrates the FIG. 9 optical system illuminating the field ofview and a heterodyne imager receiving light reflected from the scene.

FIG. 11 illustrates a waveguide configuration that uses multiple ringsor racetrack waveguides to implement a spectral filter.

FIG. 12 illustrates how different local oscillator signals are generatedfor different regions of the heterodyne imager field of view. The laserdiode spectrum is separated into multiple local oscillator signals usingwaveguide ring resonators.

FIG. 13 is a system block diagram showing the interaction of the variouscomponents and functions that comprise the invention of a secondembodiment.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

Any reference to “invention” or the specific invention name “HSAAI”within this document is a reference to an embodiment of a family ofinventions, with no single embodiment including features that arenecessarily included in all embodiments, unless otherwise stated.Furthermore, although there may be references to “advantages” providedby some embodiments, other embodiments may not include those sameadvantages, or may include different advantages. Any advantagesdescribed herein are not to be construed as limiting to any of theclaims.

Specific quantities, dimensions, spatial characteristics, compositionalcharacteristics and performance characteristics may be used explicitlyor implicitly herein, but such specific quantities are presented asexamples only and are approximate values unless otherwise indicated.Discussions and depictions pertaining to these, if present, arepresented as examples only and do not limit the applicability of othercharacteristics, unless otherwise indicated.

In describing preferred and alternate embodiments of the invention,specific terminology is employed for the sake of clarity. The technologydescribed herein, however, is not intended to be limited to the specificterminology so selected, and it is to be understood that each specificelement includes all technical equivalents that operate in a similarmanner to accomplish similar functions.

The drawings use a combination of electrical symbols, logic symbols andpictorial representations to illustrate the elements of the invention.In the interest of clarity, the symbols are simplified and do notexplicitly show unneeded detail.

Example embodiments will now be described more fully with reference tothe accompanying drawings of the invention. Specific details are setforth such as examples of specific components and methods to provide athorough understanding of embodiments of the present disclosure. It willbe apparent to those skilled in the art that specific details need notbe employed, that example embodiments may be embodied in many differentforms, and that neither should be construed to limit the scope of thedisclosure. In some example embodiments, well-known device structuresare not described in detail.

The invention has the potential to be configured in multiple versions soas to generate superior technical performance in any given application.Therefore, it is understood that in some configurations not all elementswill always be necessary for the specific embodiment or implementationof the invention. It should also be apparent that there is norestrictive one-to-one correspondence between any given embodiment ofthe invention and the elements in the drawing.

The HSAAI invention comprises a two-dimensional array of N by M lightcollecting sites (LCS). This invention applies to any N by M array ofLCSs where N and M are integers and where either or both N and M canequal one or any large integer value.

The HSAAI heterodyning process is illustrated by the components inFIG. 1. Light sources 1 and 2 generate light signals 3 and 4 (withdifferent wavelengths) propagating through waveguides 5 and 6,respectively. The waveguides are then joined into a single waveguide 65bringing the waveguides 5 and 6 together, so that the two light signalsor light streams 3 and 4 have the same electromagnetic mode and arepolarization aligned for heterodyning within a photo detector 7. Thephoto detector 7 is a square law photo detector that heterodynes ormultiplies the light signals 3 and 4 to generate the photo detectorelectrical output signal 8.

FIG. 2 illustrates a frequency spectrum of the light signal 4 (nowreferred to as the scene light or the scene light signal) for mixing orheterodyning with the light signal 3 (now referred to as the localoscillator signal or the local oscillator light signal), the resultappearing as the photo detector output signal 8, comprising a directcurrent component 8B and a multi-frequency component 8A (also referredto as the heterodyned signal). The frequency spectrum of the heterodynedsignal is identified by a reference character 9. The existence andproperties of the frequency spectrum 9 are understood by those who areskilled in the heterodyning art. The frequency spectrum 9 is centered ata difference frequency 10, i.e., the difference between the centerfrequencies of the local oscillator signal 3 and the scene light signal4. In other words, a replica of the optical frequency spectrum of thescene light signal 4 is approximately duplicated as the frequencyspectrum of the heterodyned signal 9 centered at the differencefrequency 10 in the photo detector electrical output signal 8. Note thatthe heterodyned signal 9 would be an exact amplified andfrequency-shifted version of the frequency spectrum of the scene light 4if the local oscillator signal 3 was monochromatic.

In the FIG. 2 illustration, the bandwidth 11B of scene light signal 4 ismuch larger than a bandwidth 11A of local oscillator light signal 3.That simplifying assumption is made in order to improve light collectionefficiency, but does not represent a limitation on the invention. Atemporal bandwidth 12 required for the photo detector 7 depends on boththe difference frequency 10 between the frequencies of light streams 3and 4 plus the temporal bandwidth of the heterodyned signal 9 (which isthe bandwidth of the local oscillator signal 3 convolved with thebandwidth of the light signal 4). To the extent practical, the bandwidthof the local oscillator signal 3 is smaller than the spectral bandwidthof scene-return light signal 4 in order to maximize the amount of scenereturn light that fits within the temporal bandwidth 12 of the outputsignal 8 from the photo detector 7. Note that unlike prior art, whichsenses a phase relationship between the light streams 3 and 4, thecurrent HSAAI does not use phase information.

FIG. 3 shows the photo diode 7 and one implementation of the photo diodeoutput circuit 26. Reference numbers 21 and 22 indicate supply voltages.Circuit elements are shown to illustrate a desired function; thoseskilled in the electronics art are aware that alternative components areavailable to perform the same or similar functions. Alternating current(AC) coupling (by a capacitor 26A) is necessary to pass the heterodynedspectral bandwidth signal (8A in FIG. 2) and block the direct currentsignal (8B in FIG. 2). During a frame period, the heterodyned signal isrectified by a diode 26B (in one embodiment a metal-oxide-metal diode),and then integrated or low pass filtered by a resistor 26C and acapacitor 26D. Thus, the three functions associated with each LCS photodetector are: AC couple, rectify, and low pass filter or integrate.These functions can be implemented in a variety of ways using a varietyof components. A reset signal, reference number 23, is applied to a FET26E, and the reset operation activated to short the capacitor 26D afterthe frame signal (recall that the frame signal is derived from a numberof illuminating light pulses) is read out from the output circuit 26.

A frame signal 55 in FIG. 3 output from the output circuit 26 isbuffered and input to circuits (not shown) that provide row and columnaddressing, read logic, analog to digital conversion, and an interfaceto a digital processor or display means. Many different forms ofcircuits and components to perform these functions are known to thoseskilled in the art.

FIG. 4 illustrates a horn coupler 13 comprising a horn antenna. Thecoupler guides light from an objective lens (not shown but that gatherslight from the scene) into an input port 13B and then into a waveguidevia an output port 13A. The horn coupler can be fabricated in silicon,for example, using anisotropic etching, or can be fabricated out ofdifferent materials using appropriate fabrication techniques. The shapeof the horn is derived from Maxwell's Equations. If the optimal hornlength is excessive for the application, a plate or layer of lenslets tohelp collect scene light and increase the fill-factor can be usedbetween the objective lens and the horn coupler. The output port orbottom region 13A of the horn coupler is shaped to efficiently conductlight into a waveguide connected to the output port; the waveguide notillustrated in FIG. 4 but further described below.

FIG. 5 illustrates a Bragg grating coupler 14, an alternative to thehorn coupler 13 of FIG. 4. The grating coupler 14 comprises ridges 14Aetched into a material surface. The collecting area (the ridged portion)of the grating is angled slightly to be oriented non-parallel to the LCSarray surface in order to efficiently couple light from thescene/objective lens into the waveguide. Light from the objective lensof the system enters 14A of the Bragg grating coupler 14 and exits at anoutput 14B and then into a waveguide, which is not illustrated in FIG. 5but further described below.

FIG. 6 illustrates a Mach Zehnder interferometer 15; like the horncoupler and Bragg grating coupler, the Mach Zehnder interferometer iswell known to those skilled in the waveguide art. In the presentinvention, Mach Zehnder interferometers can be used as optical switches.Generally, a Mach Zehnder interferometer comprises two waveguides 15Aand 15B that are brought into close proximity at two regions 15C and 15Dalong their length, as can be seen in FIG. 6. FIG. 6 depicts lightintroduced at an input 15G into a waveguide 15A. Evanescent couplingoccurs at coupling regions 15C and 15D. The coupling region 15C splitsthe light such that a portion of the incident light into the waveguide15A is coupled to a waveguide 15B. At the second coupling region 15D,the phase difference of the optical signal in the two waveguides 15A and15B determines whether the light remains split or combines into eitherthe waveguides 15A or 15B. In other words, the light can be directed toeither output 15E (of the waveguide 15A) or the output 15F (of thewaveguide 15B) by controlling the relative phase (i.e., phasedifference) of the optical signal traveling in the two Mach Zehnderinterferometer waveguides 15A and 15B.

In FIG. 6, a PIN diode 17 is shown as disposed in the waveguide 15B. Theoptical path length of light in the waveguide 15B can be varied byintroducing electrical current into the PIN diode 17; that is, therefractive index of the waveguide is changed by forward biasing the PINdiode. Changing the refractive index changes the optical path length inthe waveguide 15B relative to the path length in the waveguide 15A,thereby controlling the phase difference between the two propagatingsignals and therefore controlling whether the light outputs solely fromthe waveguide 15A or the waveguide 15B or is split between the twooutputs. In effect, the PIN diode 17 functions to configure the MachZehnder interferometer as an electrically controllable optical switch.

FIG. 7 illustrates overall operation of an active imager LCS 32. A lightsource 33, a laser diode for example, generates a light signal 34 thatreflects from a scene 35 into an LCS coupler 36. (Either the horncoupler 13 of FIG. 4 or the Bragg grating 14 of FIG. 5 may be used tocollect light.) The return light (also referred to as the scene light 4)is converted to a single mode by a polarization diversifier 37 and thesingle mode scene light 4 travels into the waveguide 6. As in FIG. 1,the local oscillator source is indicated by the reference number 1, andthe local oscillator light is designated by reference number 5 travelingthrough the waveguide.

Although FIG. 7 depicts the local oscillator source 1 as proximate theLCS 32, in a preferred embodiment the local oscillator light may becarried to each LCS in the LCS array by waveguides not shown in FIG. 7.

The polarization diversifier 37 can be fabricated to transmit transversemagnetic (TM) mode radiation and convert transverse electric input (TE)mode to TM. Conversely, the diversifier 37 can also be fabricated totransmit TE by converting input TM waves to TE mode waves.

Still referring to FIG. 7, the scene light 4 and local oscillator light3 are combined in the waveguide 65. In waveguide 65, both light streamsare the same mode and highly confined. The signal propagating throughthe waveguide 65 is input to the photo detector 7 (also referred toherein as a photo diode) in ways known to those skilled in the waveguideart. Heterodyning occurs in photo detector 7 with the heterodynedelectrical output signal identified by the reference character 8 (alsoreferred to as the photo detector output signal).

The photo detector output signal 8 in FIG. 7 is AC coupled, rectified,and integrated by the photo diode output circuit 26 (as described inconjunction with FIG. 3), producing the frame signal 55.

The light source 33 in FIG. 7 is pulsed rapidly in order to range gateout reflections from nearby air aerosols and local objects that willsaturate the image and effectively hide more distant objects. Practicalrange gated imaging requires that the receiver be effectively turned offduring illuminator emission and shortly thereafter in order to avoidexcessively bright backscatter. Changing the wavelength of the localoscillator to de-sensitize the receiver provides a total solution insome cases. In other cases, when the laser return signal is large, oneof the known means commonly used with laser radars can implemented inaddition to or in lieu of changing the local oscillator wavelength.

Since each illuminator pulse contains little energy, many pulses, asreflected from the distant scene, must be integrated in capacitor 26D ofFIG. 3 before the capacitor signal is large enough to exceed any readoutnoise. That means many laser pulses from the illuminator (also referredto as a light source) are emitted and reflected from the scene, whilethe reflected signals from previous illuminator pulses are stored on thecapacitor 26D of FIG. 3. Since there is a strong return signal fromnearby objects or from air aerosols during pulse emissions from theilluminator, it is necessary to prevent any signal from reaching thecapacitor 26D when the illuminator is turned on.

That is accomplished, in one embodiment, by changing the localoscillator wavelength/frequency such that the difference frequency 10 inFIG. 2 is larger than the temporal bandwidth of the photo detector. Inother words, the heterodyned signal 9 in FIG. 2 is at a high frequencybeyond the bandwidth of the photo detector and therefore cannotcontribute to the output electrical signal 8A from the photo detector 7.

Note that the amplitude of the local oscillator is not changed when thefrequency/wavelength is changed, so that no AC coupled signal on theintegrating capacitor 26D in FIG. 2 results from shifting of the localoscillator wavelength.

Thus, during periods when the illuminator is emitting, the wavelength ofthe local signal 3 (see FIG. 2) is moved (shifted to a shorterwavelength) in order to inhibit heterodyning by shifting the heterodynesignal to a very high frequency outside of the photo diode bandwidth.When the illuminator stops emitting, the local oscillator wavelength isreturned to a wavelength close to or within the spectral bandwidth 11 ofthe scene light 4, such that heterodyned detection of reflected scenelight once again occurs.

The frame at each LCS is created by integrating many illuminator pulses.As described above, the local oscillator frequency is shifted duringeach illuminator pulse in order to prevent heterodyning and integrationof the illuminator signal. Once the illuminator is turned off, the localoscillator is returned to a wavelength that places the bandwidth 9 ofheterodyned electrical signal 8A within the temporal bandwidth of thephoto detector. See FIGS. 1 and 2. The weak reflections returning fromthe scene are heterodyned efficiently and the resultant signal is storedin the capacitor 26D (FIG. 3), pending arrival of a subsequent pulse orpulses.

After enough pulses have been summed to achieve a suitably highsignal-to-noise ratio, the frame signal 55 at each LCS site is read outby a read-out device 57 employing row and column read logic. As shown inFIG. 7, the read-out device 57 receives the frame signal 55 from eachLCS in an array (only one shown in FIG. 7) and combines the framesignals to produce an array signal 58, which depicts the entire imagedscene. When the array signal is generated, the capacitor 26D of FIG. 3is reset by applying the reset signal 23 to close the FET 26E, shortingthe capacitor 26D to ground, thereby getting the capacitor ready tobegin integrating the photo detector output signals for the next framesignal from each LCS site.

Nominal illumination duty cycle is 0.5. If the maximum range to besensed is R_(max), then the illuminator is turned on for time t_(laser)equal to 2 R_(max)/c where c is the speed of light. That is, the pulseis just long enough to reach from the HSAAI to the maximum range andback. The illuminator is then turned off for a time t_(laser) to achievethe 0.5 duty cycle.

If a dark zone in front of the HSAAI is desired, then the localoscillator wavelength is not restored to its desired wavelength forefficient heterodyning for some period longer than t_(laser). That is,the local oscillator wavelength is always shifted to stop signalintegration on capacitor 26D in FIG. 3 at the start of t_(laser).However, integration is not necessarily restored at the end of t_(laser)but can be delayed in order to not integrate light reflected from nearbyobjects. Since many pulses are integrated during each image frame,effective illumination versus range is controlled by varying the startof integration time pulse-by-pulse. That is, the dark zone in front ofthe HSAAI is varied pulse by pulse to generate the desired apparentillumination at each range.

Range from a scene object to each LCS imaging that object is found byilluminating one whole frame (FRAME_1) using a fixed time for t_(laser).For the next frame, FRAME_2, the duty cycle of the laser illuminator islinearly decreased from a 0.5 duty cycle to zero from start of frame toend of frame, respectively, while not changing the pulse stop times.That is, the series of laser pulses emitted during the second frame havetheir pulse on-times shortened by delaying the start time of eachsubsequent pulse. The range to the object reflecting light into each LCSis then R_(max) minus (LCS amplitude FRAME_2 divided by LCS amplitudeFRAME_1) multiplied by R_(max). Frame one has constant pulses of thenormal type described earlier in the application. Frame two uses pulsesthat are equal in length at the very start of the frame but the pulsewidth gets shorter as the frame goes on until the width is zero at framestop. Accuracy of range to a surface is improved by averaging overseveral or many LCS location.

FIG. 8 is similar to FIG. 7 with the addition of a Mach Zehnder opticalswitch 15 to provide additional blockage of the scene light signal 4during illuminator emission. The description of elements 1, 2, 3, 4, 5,6, 7, 8, 23, 24, 26, 33, 34, 35, 36, 37, 55, and 58 are all the same asdescribed in FIG. 7.

In FIG. 8, the Mach Zehnder optical switch 15 is added between thepolarization diversifier 37 and the waveguide 6. A current mirrorcircuit 71 is set by control lines and voltage strobes 72 to providecurrent to the pin diode 17 for accurate on and off states for thewavelength of the illuminator or light source 33. The Mach Zehnderoptical switch switches the light in waveguide 6 off when theilluminator 33 is on.

DETAILED DESCRIPTION OF THE ALTERNATIVE EMBODIMENT

The illuminator associated with the alternative embodiment of theinvention is labeled 119 in FIG. 9. The illuminator comprises a laserdiode or other light source 100 (typically regarded as broad band lightsource) that is focused on a slit 113 by lens 112 and then the light iscollimated by lens 114. The transmissive blazed (ruled) grating 115spreads the light according to rules known to those expert inspectrometer design, with shorter wavelengths to one side of the fieldof view and greater angular spread for longer wavelengths to the otherside of the field of view. Lenses 116 and 117 operate together as anafocal to adjust the angular spread of the laser diode light over thedesired field of view. The angular field of view is determined by theratio of the focal lengths of lens 116 and 117.

There are many configurations possible for spreading the opticalspectrum over the field of view, including configurations that spreadthe wavelengths in two dimensions by using crossed diffraction andechelle gratings. Various options include prisms as well as gratings,and gratings include blazed, echelle, diffraction and multiple gratingdesigns. Any of the configurations known to those who are expert inspectrometer design are appropriate and can be used in lieu of theconfiguration in FIG. 9.

FIG. 10 illustrates the FIG. 9 optical system 119 illuminating differentregions of a field of view 139 (a portion of a scene) with differentwavelengths of light 130, 131, 132, and 133. The variation inilluminator wavelength can be horizontal (as is the case in FIG. 10) orvertical or even two dimensional, depending on the configuration of theoptical components in FIG. 9.

The next several paragraphs describe additions or modifications to thepreferred HSAAI embodiment that comprise the alternative embodiment. Theadded components partially comprise spectral filters to generate theappropriate local oscillator (LO) frequencies for each region of thefield of view and also include photo diodes, electronics for signalconditioning and digitizing, and processor implementation of LOfrequency/wavelength adjustment relative to the illuminator spectrum(i.e., the scene light) arriving at each position in the HSAAI field ofview.

FIG. 11 illustrates a waveguide spectral filter 120 that uses multipleracetrack waveguides to form the needed wavelength spectrum. In FIG. 11,light from source 100 enters at end 123A of the add waveguide 123. Lightis evanescently coupled between the add waveguide 123 and the racetrackwaveguides 124; the various ring or racetrack waveguides 124 areevanescently coupled to each other at differing regions and in variousways. Changing the coupling, the dimension of each racetrack or ring, orchanging the refractive index by some method (such as by using the PINdiode as described above) changes the spectral filter characteristics.

Depending on the relationship between the light wavelength and theracetrack 124 dimensions and coupling, some wavelengths of lightresonate in the racetrack 124 while other wavelengths do not. Light inthe add waveguide 123 that resonates in the racetrack 124 exits theracetrack waveguide via the drop waveguide 125 at an end 125A. Lightthat does not resonate in the racetrack 124 exits the add waveguide 123at an end 123B and can then be connected to an add waveguide of asubsequent spectral filters.

In FIG. 11, light that enters a drop waveguide 125 at end 125B andresonates in the combination of racetracks 124 will, by symmetry, exitthe waveguide 123 at the end 123B. Light entering the waveguide 125 atend 125B that does not resonate in racetracks 124 exits the waveguide125 at end 125A. Thus, many spectral filters 120 can be connected inseries to generate filtered spectral bands.

In FIG. 11, the PIN diode 126 with electrical inputs 126A and 126B canbe used to control the waveguide refractive index and therefore thespectral properties of the filter 120. The refractive index is changedby passing current through the PIN diode. PIN diode current is providedand controlled by a current source 127 with current amplitude inputsignal 128 and latch input signal 129. Some spectral filters requiremultiple PIN diodes and associated current sources and controls. Thediode P+ and N+ regions often encompass the space inside and justoutside the ring or racetrack in order to make the diode large andincrease the effect of diode current on the refractive index. Analternative is to place a small heating element under the spectralfilter 120 and control the refractive index by changing the temperature.The PIN diode implementation is used in the preferred embodiment. Anynumber of rings or racetracks with or without PIN diodes can be used toimplement a spectral filter.

In FIG. 12, the local oscillator light from a laser diode 141 or anotherlight source is split into multiple paths by a waveguide splitter 138.The light source 141 can also be fiber optically coupled light from theilluminator. Spectral plot 130 of the input light shows amplitude on theordinate and wavelength on the abscissa axes. The input light isspectrally filtered by a spectral filter 123 resulting in light with aspectrum 133 output as local oscillator light 143 to some portion of aheterodyne focal plane array. Light that is not in the spectral band ofthe spectral filter 123 passes to a series of spectral filters, one ofwhich is 126. Within the spectral filter 126, local oscillator light 146has spectrum 136. Photo diode 144 senses the amount of light that hasnot been diverted to a spectral filter between the light source 141 andthe photo diode 144. Photo diode 144 is used to help align and then helpin maintaining alignment of LO and illuminator light source wavelengths.

The output signal from each spectral filter 123, 126, and additionalfilters not shown, can be determined by activating just one spectralfilter at a time and sensing the drop in the output signal 145 from thephoto diode 144. By sensing the signal amplitude using photo diode 144,the LO and illuminator wavelengths are maintained in a suitablerelationship for heterodyning.

FIG. 13 illustrates an array 150 of light collection sites (LCS) 101.The array 150 receives illuminator light scatted back from the scene andheterodynes that light with local oscillator signals to form an image.The operation of a heterodyne imager is known to those skilled in theart, is also described above in the preferred embodiment, and is notfurther described here.

The illuminator described by FIG. 9 and FIG. 10 provides light that hasa small enough spectral bandwidth to heterodyne efficiently at eachpoint in the scene. However, the wavelength of the illuminator lightvaries over the field of view. In FIG. 13, an array 110 of spectralfilters 120 is added to the heterodyne array 100 in order to generatelocal oscillator signals that align properly with the illuminator lightat each separate location in the field of view. (Aligning properlyrequires that the local oscillator light be close in wavelength to oneedge of, but not too far into, the illuminator spectral band.)

A digital processor 200 in FIG. 13 provides many functions for theactive imager; important here is that the processor has access to thesignal image outputs of all LCS 101 in FIG. 13. The LCS are oftenreferred to as pixels in the general case. The processor 200 also readsthe photo diode output signals 145 in FIG. 12 and calculates andcontrols the spectral electrical inputs 128 and 129 to the PIN diode 127in each spectral filter 120.

FIGS. 9, 10, and 13 illustrate one implementation where the light of thesame wavelength is distributed vertically, while the wavelength changeshorizontally over the field of view. However, optical distortion andaberrations and minor differences in the illuminator and imager opticscan create an irregular pattern of illuminator wavelength over the fieldof view. In an embodiment where the wavelength is the same vertically,perfect optics and illuminator and imager axes alignment would result inthe same local oscillator wavelength along each column of LCS in FIG.13. In order to accommodate realistic tolerances, multiple spectralfilters 120 are implemented (in this case four) for each column of LCS.That number of spectral filters will of course vary depending on manytolerance and design factors.

Further, the wavelength of the light from source 141 will undoubtedly betemperature, time, and production-tolerance dependent; the wavelengthwill vary from unit to unit and for each unit from time to time. Thefields of view of both the illuminator and receiver can optionally bebuilt larger than necessary to accommodate variation in the illuminatorspectrum.

Local oscillator spectral bandwidth for each spectral filter 120 isfound by design. Local oscillator center wavelength is found by signalprocessing in the digital processor 200 of FIG. 13. For each of manyspectral filters, the processor sums the signal from all of the LCSserved by a particular spectral filter 120. The search for maximumsignal can happen quickly because adjacent regions of the field of viewwill be illuminated by nearly the same wavelength of light.

What is claimed is:
 1. A heterodyne starring array active imager forproducing an image of a scene, the heterodyne starring array activeimager comprising: a first light source operating as an illuminator ofthe scene; a component for segregating light from the light source intoa plurality of frequency bands or wavelength bands, each band forilluminating a region of the scene; an array of light collecting sitesfor imaging the scene, each one of the light collecting sitescomprising: a coupling component for optically coupling scene light intoa scene light waveguide; a second light source for emitting localoscillator light; an array of waveguide spectral filters for tailoringthe local oscillator light for each region of a field of view, such thatthe local oscillator light for each region has a specific bandwidth; anarray of local oscillator light waveguides to distribute the localoscillator light to each region of the array of light collecting sites;the scene light waveguide and local oscillator waveguides coupled to athird waveguide, the scene light and the local oscillator light mergingand propagating into the third waveguide; a square law photo detectorfor receiving light propagating in the third waveguide, whereinheterodyning of the scene light and the local oscillator light occurs atthe photo detector to produce a photo detector output signal; componentsfor processing and integrating a plurality of the photo detector outputsignals from each light collecting sight to produce a frame signal; anda read-out device producing an array signal responsive to the framesignal from each light collecting site.
 2. The heterodyne starring arrayactive imager of claim 1, wherein the component for segregating lightcomprises a diffraction grating dispersing the light horizontally,vertically, or at some angle diagonally across the portion of the scenewithin the imager field of view.
 3. The heterodyne starring array activeimager of claim 2, wherein the diffraction grating comprises a prism. 4.The heterodyne starring array active imager of claim 1, wherein thefirst light source comprises a laser diode emitter, a light emittingdiode, a quantum emitter, a thermal emitter, or an arc lamp, and whereinthe second light source comprises a laser diode emitter, a lightemitting diode, a quantum emitter, a thermal emitter, or an arc lamp. 5.The heterodyne starring array active imager of claim 1, wherein thefirst light source illuminates the scene with a spectral bandsufficiently narrow to allow use of a single local oscillator frequencyband for each region of the field of view.
 6. The heterodyne starringarray active imager of claim 1, wherein the coupling component comprisesa horn coupler or a Bragg grating coupler.
 7. The heterodyne starringarray active imager of claim 1, wherein a material of the horn coupleror the Bragg grating coupler comprises silicon.
 8. The heterodynestarring array active imager of claim 1, further comprising apolarization diversifier for converting the scene light to a singlemode, the polarization diversifier disposed between the couplingcomponent and the scene light waveguide.
 9. The heterodyne starringarray active imager of claim 1, wherein the first light source comprisesa continuous laser light source with a gate to provide gated control ofillumination to intermittently illuminate the scene, and wherein thegated control is adjustable to provide different range gate settings.10. The heterodyne starring array active imager of claim 1, wherein awavelength of the local oscillator light is shifted when the lightsource is illuminating the scene such that a difference frequency equalto a frequency of the scene and a frequency of the local oscillatorlight is outside a bandwidth of the square law photo detector when thelight source is illuminating the scene.
 11. The heterodyne starringarray active imager of claim 1, wherein the components for processingand integrating comprise components for AC coupling, rectifying, and lowpass filtering or integrating the photo detector output signal toproduce the frame signal.
 12. The heterodyne starring array activeimager of claim 1, wherein the first light source comprises a pulsedlight source.
 13. The heterodyne starring array of claim 1, whereinheterodyning of the scene light and the local oscillator light isintermittent due to intermittent illumination of the scene or due toshifting a wavelength of the local oscillator light, wherein a range tothe scene is determined during intermittent periods using a time offlight technique.
 14. The heterodyne starring array active imager ofclaim 1, further comprising a waveguide Mach Zehnder component forpreventing the scene light from entering the first waveguide when thelight source is illuminating the scene.
 15. The heterodyne starringarray active imager of claim 1, wherein the component segregates thelight source such that vertically aligned regions of the scene areintermittently illuminated by light from a same frequency band orhorizontally aligned regions of the scene are intermittently illuminatedby light from a same frequency band.
 16. The heterodyne starring arrayactive imager of claim 1, wherein the array of light collecting sitescomprises an N×M array of light collecting sites where N and M areinteger values.
 17. The heterodyne starring array active imager of claim1, wherein the scene light and the local oscillator light are of thesame mode.
 18. The heterodyne starring array active imager of claim 1,wherein intermittently illuminating the light source comprises blockinglight from the light source, and wherein integrating by the componentsdoes not begin until a period of time after illuminating the scene hasended.
 19. The heterodyne starring active array imager of claim 1,wherein a spectral bandwidth of the local oscillator light is smallerthan a spectral bandwidth of the scene light.
 20. A heterodyne starringarray active imager for producing an image of a scene, the heterodynestarring array imager comprising: a laser light source; a component forsegregating light from the light source into a plurality of wavelengthbands, each band for intermittently illuminating a region of the sceneby operation of an adjustable range gate; wherein intermittentlyilluminating the light source comprises pulsing the light source on andoff, and wherein for a first frame a duty cycle of the on and off pulsesis 0.5, and wherein during subsequent frames the duty cycle is reducedto 0; an N×M array of light collecting sites imaging the scene, whereinN and M are integers, each one of the light collecting sites comprising:a coupling component further comprising a horn coupler or a Bragggrating coupler for optically coupling scene light into a firstwaveguide; a Mach Zehnder interferometer disposed between the couplingcomponent and a first waveguide, the Mach Zehnder interferometeroperating as an optical switch; a polarization diversifier forconverting the scene light to a single mode, the polarizationdiversifier disposed between the Mach Zehnder and the first waveguide; alocal oscillator light coupled into a second waveguide, wherein aspectral bandwidth of the local oscillator light is smaller than aspectral bandwidth of the scene light; the first and second waveguidescoupled to a third waveguide, the scene light and the local oscillatorlight merging and propagating into the third waveguide; a square lawphoto detector for receiving light propagating in the third waveguide,wherein heterodyning of the scene light and the local oscillator lightoccurs at the photo detector to produce a photo detector output signal;wherein while the light source illuminates the scene, a wavelength ofthe local oscillator light is changed such that a difference frequencyof the local oscillator light and the scene light is outside a temporalbandwidth of the square law photo detector; components for AC coupling,rectifying, and low pass filtering or integrating a plurality of thephoto detector output signals to produce a frame signal; and a read-outdevice producing an array signal responsive to the frame signal fromeach light collecting site.